ISO 10296:1992 PDF

Name: ISO 10296:1992 — Aircraft — Hybrid remote power controllers — General requirements
SKU: ISO 10296:1992
Price: 25 EUR
Availability: InStock

Aircraft — Hybrid remote power controllers — General requirements

Название (английский):

ISO 10296:1992

Aircraft — Hybrid remote power controllers — General requirements

Статус документа:: Действующий
Формат:: Электронный (PDF)
Количество страниц:: 11
Дата публикации:: 23 июля 1992 г.
Издание:: ISO IS 10296 edition 1 version 1
ICS:: 49.060

Тип поставки:

Full version165 €Read online 24h10 €Read online 72h15 €

Язык документа:

ruen

Срок поставки:2 раб. дн. (перевод)

Цена:165 €

Описание (английский):

Specifies the general design and performance requirements. The controllers consist of an electromagnetic device or a combined electromagnetic/solid-state device for load switching, and a solid-state control circuit for control of the load-switching devices. On aircraft, they are used to close and open the electrical circuit and to protect wiring and equipment in the event of overload or short-circuit conditions.

Abstract

Похожие стандарты

Упомянутые в описании и другие стандарты ISO

Overview

ISO 10296:1992 - Aircraft - Hybrid remote power controllers - General requirements - defines the general design and performance requirements for hybrid remote power controllers used on aircraft. These devices combine an electromagnetic (or combined electromagnetic/solid‑state) load‑switching element with a solid‑state control circuit to open/close electrical circuits and protect wiring and equipment against overloads and short circuits. The standard covers materials, construction, terminals, enclosures, mounting, control/status signals, operating behaviour and qualification/testing considerations.

Key topics and technical requirements

Scope & definitions: Clear definitions for remote power controller, hybrid remote power controller and trip‑free operation (requires reset after a trip).

Controller types: Two basic designs:

Type A - electromagnetic device performs the load switching; control circuit drives the contactor coil.
Type B - solid‑state switch performs the main make/break function; electromagnetic contacts carry current or break fault currents as required.

Materials & construction: Non‑combustible materials that do not emit harmful gases or form conductive paths under test conditions; parts should support a practical shelf life (ideally ~20 years) unless otherwise declared.

Terminals & mounting: Requirements for stud and plug‑in terminals, terminal barriers/covers, and threaded stud strength. Studs must accommodate hardware and retain minimum thread engagement; plug‑ins require gold over nickel plating where applicable.

Enclosures & sealing: Three enclosure styles - ventilated explosion‑proof, hermetically sealed, and environmentally sealed (non‑hermetic) - with fill/gas and pressure guidelines for sealed units.

Control & status signals: Inputs may include 28 V d.c. nominal, grounded control, TTL/CMOS logic or multiplexed impedance/status. Output status signals must indicate ON/OFF and recommended trip/fault indications; in Type B the contact state and solid‑state state must be represented (status timing error ≤ 10 ms).

Operational behavior: Controllers must detect overcurrents, short circuits and phase imbalance (for three‑phase units), include a trip‑free feature, and operate across specified electrical/mechanical steady‑state and transient conditions.

Environmental & qualification testing: References established environmental test procedures for airborne equipment.

Practical applications and users

Typical users: avionics engineers, aircraft systems designers, OEM manufacturers of circuit protection and power distribution, certification authorities, and maintenance/repair organizations.

Applications: Primary protection and remote switching of aircraft loads (avionics, electrical buses, motors, lighting), integration with aircraft control buses, modular power distribution panels, and retrofit/upgrades where reliability and fault isolation are required.

Related standards

Normative references cited in the document include ISO 7137:1987 (aircraft environmental conditions and test procedures) and environmental/insulation test standards referenced for aircraft electrical equipment. Use ISO 10296:1992 together with current IEC/ISO electrotechnical and airborne equipment test standards when designing, qualifying or certifying aircraft power controllers.

ISO 10296:1992 PDF

Abstract

Похожие стандарты

Overview

Key topics and technical requirements

Practical applications and users

Related standards

Технические детали

ISO 7137:1987

Aircraft — Environmental conditions and test procedures for airborne equipment

ISO 8689-1:2000

Water quality — Biological classification of rivers — Part 1: Guidance on the interpretation of biological qu…

ISO/ASTM51540-04(2012)

Standard Practice for Use of a Radiochromic Liquid Dosimetry System (Withdrawn 2020)

ISO/ASTM51204-04

Standard Practice for Dosimetry in Gamma Irradiation Facilities for Food Processing (Withdrawn 2013)

ISO/ASTM51431-05

Standard Practice for Dosimetry in Electron Beam and X-Ray (Bremsstrahlung) Irradiation Facilities for Food P…

ISO/ASTM52628-20e1

Standard Practice for Dosimetry in Radiation Processing

ISO/ASTM52921-13(2019)

Standard Terminology for Additive Manufacturing—Coordinate Systems and Test Methodologies

ISO/ASTMTR52917-EB

Additive Manufacturing — Round Robin Testing — General Guidelines